Lockheed F-104 Starfighter vs. Mitsubishi A6M Zero

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Lockheed F-104 Starfighter versus Mitsubishi A6M Zero
16.69 m 54 ft 9 in length 9.06 m 29 ft 9 in
4.11 m 13 ft 6 in height 3.05 m 10 ft
6.68 m 21 ft 11 in wingspan 12 m 39 ft 4 in
1 Turbojet Engine engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
46.7 / 71.2 kN (dry/with Afterburner) thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
46.7 / 71.2 kN (dry/with Afterburner) total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
13,500 kg 29,800 lb MTOW 2,800 kg 6,170 lb
1,200 km 648 nm range 1,010 nm 1,871 km
510 mph 821 km/h cruise speed 180 knots 105 mph
capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.